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    Summary of recent investigations of inlet flow distortion effect on engine stability (1974)
    In:  CASI
    Details
    Publication Date: 2019-07-13
    Description: A review is presented of recent experimental results, analytical procedures and test techniques employed to evaluate the effects of inlet flow distortion on the stability characteristics of representative afterburning turbofan and turbojet compression systems. Circumferential distortions of pressure and temperature, separately and in combination are considered. Resulting engine sensitivity measurements are compared with predictions based on simplified parallel compressor models and with several distortion descriptor parameters.
    Keywords: PROPULSION SYSTEMS
    Type: NASA-TM-X-71505 , E-7878 , Aerospace Sci. Meeting; Jan 30, 1974 - Feb 01, 1974; Washington, DC; United States
    Format: application/pdf
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